CN102214518B - Structure of array type tandem solar battery module and manufacturing method thereof - Google Patents
Structure of array type tandem solar battery module and manufacturing method thereof Download PDFInfo
- Publication number
- CN102214518B CN102214518B CN201010156529A CN201010156529A CN102214518B CN 102214518 B CN102214518 B CN 102214518B CN 201010156529 A CN201010156529 A CN 201010156529A CN 201010156529 A CN201010156529 A CN 201010156529A CN 102214518 B CN102214518 B CN 102214518B
- Authority
- CN
- China
- Prior art keywords
- solar cell
- cell module
- type solar
- concatenation type
- module according
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
- Y02E10/549—Organic PV cells
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Landscapes
- Photovoltaic Devices (AREA)
Abstract
The invention discloses a structure of an array type tandem solar battery module. The structure comprises a transparent substrate, a transparent conducting film, one or more conducting substrates, a catalyst layer, photosensitive dye and a hole transport layer, wherein the transparent conducting film is formed on the transparent substrate which is used as the cathode of a solar battery module, and the transparent conducting film is regionalized into a plurality of separated regions; the surface of each conducting substrate is provided with an electron transport layer with one or more regions which are matched with the plurality of separated regions, the electron transport layer consists of a plurality of semiconductor nanotubes, and the conducting substrate with the electron transport layer is used as the anode of the solar battery module; the catalyst is formed on the cathode; the photosensitive dye is attached to the tube walls of the semiconductor nanotubes; and the hole transport layer is arranged between the cathode and the anode.
Description
Technical field
The invention relates to the how array concatenation type solar cell module of mitron technology manufacturing of a kind of utilization, especially about a kind of solar cell module that utilizes the series/parallel in block anode region and cathodic region.
Background technology
In the face of the energy crisis and the problem of environmental pollution that raise day by day, it is flourish to make that renewable energy resources industry miscellaneous begins, for example, and solar energy, wind energy and living mass-energy etc.Wherein, solar cell is considered to the most potential renewable energy resources, and therefore, also grow up just with surprising rapidity in its world market.In the middle of several at present known solar cells; First generation solar cell is to be the list of main material/compound crystal silicon solar cell with silicon (Si); It can reach the photoelectric conversion efficiency of 12-20%; Be the main holder in present solar cell market, its main application is to be applied on the power supply and construction solar power generation module of portable electronic product.The essential structure of first generation solar cell is the combination of P/N N-type semiconductor N; When irradiation; Electronics is excited and produces the shunting in electronics and electric hole; Under the influence that receives inner potential, attracted by N type and P type semiconductor respectively and accumulate in the two ends of element, derive via external circuit again and form electric current.Its advantage is to have quite high photoelectric conversion efficiency, but shortcoming is that process conditions strictness and manufacturing cost are high.
Second generation solar cell is inorganic semiconductor film (thin film) solar cell; It comprises amorphous silicon (a-Si; Amorphous silicon) solar cell and compound semiconductor film battery; For example: cadmium telluride (CdTe), GaAs (GaAs) and copper indium gallium selenide (CIGS, copper indium gallium selenide).Though the photoelectric conversion efficiency of hull cell is many to be low than the silicon wafer solar cell, material cost is also cheap relatively, and it is the minimum commercialization solar cell of present cost, is used in the consumption electronic products more.The advantage of this based thin film solar cell is that the spectral absorption scope is wide, and has thermal stability preferably, but employed heavy metal has serious injury to environment in the material, therefore still must actively seek alternative.Wherein, The III-V compound semiconductor material that the CIGS thin-film solar cells is made up of CIGS constitutes; It is to utilize common evaporation coating technique to prepare an absorbing layer film; Thickness only needs＜3 μ m, on manufacturing cost, is low than the silicon wafer solar cell therefore, and can reaches the photoelectric conversion efficiency near 20%.
What attract most attention at present should belong to third generation novel solar battery, and its aim prepares low-cost and high efficiency solar cell for importing novel materials and innovative technology, hopes the introduction through new construction, and reaches the purpose that increases photoelectric conversion efficiency.Mainly can be divided into the organic conductive macromolecule or the solar battery structure of novel how rice material.For example; Utilize the macromolecular solar battery of organic polymer as the transform light energy media; Its conversion efficiency is from below 1% of beginning; Be promoted to 5～6%, macromolecular solar battery has advantages such as light weight, deflection characteristic, processing procedure environmental protection, low cost of manufacture and high application, is to belong in the emerging solar cell of the third generation to have a kind of of potentiality.Another kind of novel solar battery then be wide can gap semiconductor the how introduction of meter structure; In conjunction with photosynthetic notion; With the transparent conducting glass is base material, on it coating one deck tool how porousness zinc oxide or the titanium dioxide semiconductor film of rice structure as work electrode, because this porous film has high surface area; Can electronics promptly be passed to semiconductive thin film and export to external circuit after absorbing luminous energy so as to making light-sensitive material at surface attachment one deck light-sensitive material.The highest energy conversion efficiency can reach 12% at present; Though efficient is not as good as the silicon wafer solar cell; But have low-cost and the easy advantage of processing procedure; And can carry out the preparation of large tracts of land and bendable cell device, and the breakthrough development of this kind has received the great attention of research unit and industry, and will develop into the main flow of solar battery technology of new generation future.
Along with the lifting of anodizing process (Anodization) technology, how the exploitation of mitron titanium dioxide (NT-TiO2) film reaches its maturity, and how this impel also that the research of mitron solar cell receives general attention in educational circles.Because the easy characteristic of NT-TiO2 thin film manufacture process, the good NT solar cell of industry will become the optimum structure of continous way volume to volume (roll to roll) solar energy in large area cell device future.How grain of rice solar cell has the following advantages in comparison for the NT solar cell of new construction and tradition: the how mitron array of (1) one dimension chromatograph that can not need loose can increase the collection efficiency of light; (2) how shunt in the mitron in electronics and electric hole, combines probability low again; (3) how electrolyte be packaged in the mitron not easy to leak, component life thereby prolongation; (4) the anodizing process processing procedure is simple and easy, can reduce the processing procedure cost of solar cell; (5) how the mitron anode has the deflection characteristic.The NT-solar cell device is altogether by three main component (Ti/TiO
2Anode, electrolyte and Pt/TCO negative electrode) form, so element has comprised Ti/TiO
2, Ti/ electrolyte, TiO
2Interfaces such as/electrolyte, Pt/ electrolyte.
Summary of the invention
Of the present invention one implements the structure that the appearance attitude can provide a kind of array concatenation type solar cell module, comprises: a transparency carrier; One transparent conductive film is formed on this transparency carrier, and wherein this transparent conductive film is changed into a plurality of separated regions by block, and will be formed with the negative electrode of this transparency carrier of this transparent conductive film as a solar cell module on it; One or more electrically-conductive backing plate; Go up one or more regional electron transfer layer of formation in its surface; Wherein one or more zone of this electron transfer layer is complementary with these a plurality of separated regions; This electron transfer layer is that how mitron constitutes by the complex root semiconductor, and will be formed with the anode of this electrically-conductive backing plate of this electron transfer layer as this solar cell module on it; One catalyst layer is formed on this negative electrode; One light-sensitive coloring agent is attached to this semiconductor how on the tube wall of mitron; And an electric hole transport layer, be arranged between this negative electrode and this anode.
Of the present invention another implemented the method for packing that the appearance attitude can provide a kind of array concatenation type solar cell module, comprises the following step: an electric hole transport layer is arranged between the anode and negative electrode of an array series solar energy battery modules; This anode and this negative electrode are bonded together, so that this solar cell module has sandwich construction; And cover a silica gel layer at the outer surface of this solar cell module.
Of the present invention another implements the manufacturing approach that the appearance attitude can provide a kind of array concatenation type solar cell module again, comprises the following step: on a transparency carrier, form a transparent conductive film; This transparent conductive film block is changed into a plurality of separated regions, wherein will be formed with the negative electrode of this transparency carrier of this transparent conductive film on it as a solar cell module; On the surface of one or more electrically-conductive backing plate, form one or more regional electron transfer layer; Wherein one or more zone of this electron transfer layer is complementary with these a plurality of separated regions; This electron transfer layer is that how mitron constitutes by the complex root semiconductor, and will be formed with the anode of this electrically-conductive backing plate of this electron transfer layer as this solar cell module on it; Make a light-sensitive coloring agent be attached to this semiconductor how on the tube wall of mitron; One catalyst layer is formed on this negative electrode; One electric hole transport layer is arranged between this negative electrode and this anode; And this anode and this negative electrode be bonded together.
According to the present invention, can produce concatenation type DSSC module with the demand of current value according to output voltage with the form of series connection or parallel form.
Of the present invention other implement detailed description that appearance attitude and advantage can combine from alterations following and in order to illustration principle of the invention example and more obvious in vain.
Description of drawings
In alterations of the present invention, components identical is represented with the components identical symbol.
Fig. 1 shows the drawing in side sectional elevation according to the concatenation type DSSC module of the first embodiment of the present invention;
The vertical view of the cathode portion of the solar cell module of Fig. 2 a displayed map 1;
Fig. 2 b shows along the drawing in side sectional elevation of the a-a line of Fig. 2 a;
The vertical view of the anode part of the solar cell module of Fig. 3 a displayed map 1;
Fig. 3 b shows along the drawing in side sectional elevation of the b-b line of Fig. 3 a;
Fig. 4 is the entity photo of the concatenation type DSSC module of Fig. 1;
Fig. 5 is the efficient chart of solar cell module after encapsulation of Fig. 4;
Fig. 6 shows the drawing in side sectional elevation according to the concatenation type DSSC module of the second embodiment of the present invention;
The vertical view of the cathode portion of the solar cell module of Fig. 7 a demonstration displayed map 6;
Fig. 7 b shows along the drawing in side sectional elevation of the c-c line of Fig. 7 a;
The vertical view of the anode part of the solar cell module of Fig. 8 a displayed map 6;
Fig. 8 b shows along the drawing in side sectional elevation of the d-d line of Fig. 8 a;
Fig. 9 is the entity photo of the concatenation type DSSC module of Fig. 6; And
Figure 10 is the efficient chart of solar cell module after encapsulation of Fig. 9.
[main element symbol description]
100 DSSC modules
110 transparency carriers
120 transparent conductive film oxide layers
121 irrigation canals and ditches
130 auxiliary electrodes
140 the moon/anodic bonding material
150 electric hole transport layers
160 electron transfer layers
170 electrically-conductive backing plates
200 DSSC modules
210 transparency carriers
220 transparent conductive film oxide layers
221 irrigation canals and ditches
230 auxiliary electrodes
240 the moon/anodic bonding material
250 electric hole transport layers
260 electron transfer layers
270 electrically-conductive backing plates
Embodiment
Below will embodiments of the invention be described, and these embodiment are merely exemplary and non-limiting through the example mode.
First embodiment
Fig. 1 shows the drawing in side sectional elevation according to the concatenation type DSSC module 100 of the first embodiment of the present invention.DSSC module 100 is a kind of tandem DSSC module.DSSC module 100 comprises: transparency carrier 110, transparent conductive film oxide layer 120, auxiliary electrode 130, the moon/anodic bonding material 140, electric hole transport layer 150, electron transfer layer 160 and electrically-conductive backing plate 170.Electricity hole transport layer 150 can contain iodide ion, and the kenel of electric hole transport layer 150 can comprise: liquid, colloidal state or solid-state.The material of electrically-conductive backing plate 170 can be indium (In), zinc (Zn), tin (Sn), titanium (Ti) or tungsten (W).The moon/anodic bonding material 140 can be a kind of plasticity molecular film, for example heat shrinkage film, thermosetting film, thermoplastic film, ultraviolet light polymerization film or pellosil.
On electrically-conductive backing plate 170, form electron transfer layer 160; And will be formed with the anode of the electrically-conductive backing plate 170 of electron transfer layer 160 on it as DSSC module 100; In wherein; Electron transfer layer 160 is that how mitron constitutes by the complex root semiconductor, making light-sensitive coloring agent (not shown) attached to after these semiconductors are how on the tube wall of mitron, can make its source of supply that becomes electronics and delivering path.This light-sensitive coloring agent can be organic metal dyestuff, inorganic light-sensitive coloring agent or organic photosensitive dyestuff.Can pass through infusion method, method of spin coating or drape process, make light-sensitive coloring agent attached to these semiconductors how on the tube wall of mitron.For example, the material that is suitable as the electron transfer layer 160 of anode can be silicon dioxide (SiO
2), indium sesquioxide (In
2O
3), tungstic acid (WO
3), zirconium dioxide (ZrO
2), zinc oxide (ZnO) or tin ash (SnO
2).For instance; A kind of mode that forms electron transfer layer 160 is: through sol-gel process, hydro thermal method, anodizing process, chemical vapour deposition technique or physical vaporous deposition; The semiconductor that directly on the surface of electrically-conductive backing plate 170, forms above-mentioned oxide is mitron how, and then makes light-sensitive coloring agent attached to these how on the mitron.In addition; The another kind of mode that forms electron transfer layer 160 is: through method of spin coating, sedimentation or spread coating; The semiconductor that makes above-mentioned oxide is how on the surface of mitron attached to electrically-conductive backing plate 170; And then make light-sensitive coloring agent attached to these semiconductors how on the mitron, at this moment, electrically-conductive backing plate 170 can be metal or nonmetallic electrically-conductive backing plate.In addition, can make these how adhere to how rice particle (for example titanium dioxide how rice particle) of semiconductor in the pipe of mitron.
Through sol-gel process, hydro thermal method, anodizing process, chemical vapour deposition technique or physical vaporous deposition; Transparent conductive film oxide layer 120 is formed on the transparency carrier 110, and will be formed with the negative electrode of the transparency carrier 110 of transparent conductive film oxide layer 120 on it as DSSC module 100.Generally speaking, transparency carrier 110 and transparent conductive film oxide layer 120 can be transparent or semitransparent material.For instance; The material that is suitable as transparent conductive film oxide layer (or being called transparent conductive film) 120 can be indium tin oxide (ITO; Indium tin oxides), aluminium zinc oxide (AZO; Al-Znoxides), antimony tin oxide (ATO, antimony doped tin oxides) or fluorine tin-oxide (FTO, fluorine doped tin oxides); And transparency carrier 110 can be the transparency carrier of transparent glass substrate, transparent plastic substrate or the like.For example, this plastic base can be made by PEN (PEN, poly (ethylene naphthalate)) or PET (PET, poly (ethyleneterephthalate)).
In DSSC module 100; Light can be seen through electric hole transport layer 150, and exposed to anode electron transfer layer 160 by transparency carrier 110 and transparent conductive film oxide layer 120; Light-sensitive coloring agent can be passed to electron transfer layer 160 rapidly with electronics after absorbing luminous energy; Be passed to electrically-conductive backing plate 170 again via electron transfer layer 160 then, see through external circuit (no icon) afterwards, and reach the transparent conductive film oxide layer 120 that promotes electronic conductivity by the auxiliary electrode (conductivity or corrosion stability metal) 130 of low resistance fast; Get back to electric hole transport layer 150 at last, to accomplish the electric transmission loop of this solar cell module.
The vertical view of the cathode portion of the solar cell module 100 of Fig. 2 a displayed map 1; And Fig. 2 b shows along the drawing in side sectional elevation of the a-a line of Fig. 2 a.Shown in Fig. 2 a and 2b, the cathode portion of solar cell module 100 comprises transparency carrier 110, transparent conductive film oxide layer 120 and auxiliary electrode 130.The generation type of this cathode portion is: on transparency carrier 110, form transparent conductive film oxide layer 120 earlier; Utilize chemical etching, laser carved or mode (be referred to as and scrape channel process) such as strike off then; On transparent conductive film oxide layer 120, form irrigation canals and ditches 121; On monolithic transparency carrier 110, to obtain to appear the transparent conductive film oxide layer 120 of K separated region (it can form array pattern); That is, transparent conductive film is changed into a plurality of separated regions by block, then; Utilize modes such as wire mark, plating, electroless plating, electrophoresis, vapor deposition, brush plating, brushing or rotary coating, auxiliary electrode 130 is formed on the edge of the negative electrode of solar cell module 100.Again, another kind of mode capable of using is made this cathode portion, promptly; Utilize masking method; Specifically, can utilize vacuum adhesive tape or mould earlier, the zone that forms transparent conductive film oxide layer 120 of not expecting on the transparency carrier 110 is covered; And then formation transparent conductive film oxide layer 120; Then remove vacuum adhesive tape or mould, can produce zone that is formed with transparent conductive film oxide layer 120 and the zone that is not formed with transparent conductive film oxide layer 120, then; Utilize modes such as wire mark, plating, electroless plating, electrophoresis, vapor deposition, brush plating, brushing or rotary coating, auxiliary electrode 130 is formed on the edge of the negative electrode of solar cell module 100.Then; Through sol-gel process, hydro thermal method, anodizing process, chemical vapour deposition (CVD), physical vapour deposition (PVD), vapor deposition or mode such as electroless plated; On the negative electrode of DSSC module 100, form catalyst layer (not shown); To promote electrochemical reaction, the material of this catalyst layer can be Au (gold), Pd (palladium), Pt (platinum) or carbon (C).This catalyst layer can have island or granular microstructure.Auxiliary electrode 130 can be conductivity or corrosion stability metal, for example copper, gold, platinum, silver, aluminium, nickel, titanium, cobalt, tin, indium or zinc.
The vertical view of the anode part of the solar cell module 100 of Fig. 3 a displayed map 1; And Fig. 3 b shows along the drawing in side sectional elevation of the b-b line of Fig. 3 a.Shown in Fig. 3 a and 3b, the anode part of solar cell module 100 comprises electron transfer layer 160 and electrically-conductive backing plate 170.This anode part is: preparation quantity can with the corresponding plural conductive substrate 170 of the separated region quantity of cathode portion, and on the surface of these electrically-conductive backing plates, formed the zone of the electron transfer layer 160 that can be complementary with the separated region of cathode portion.At last; On the negative electrode of DSSC module 100 and the interface between the anode, the moon/anodic bonding material 140 is set and makes negative electrode and anodic bonding together; And the electric hole transport layer 150 contain iodide ion is set between negative electrode and anode; Can accomplish the encapsulation of concatenation type DSSC module 100 and make it have sandwich construction (that is, utilizing Sanming City therapy to encapsulate), as shown in Figure 1.The set-up mode of electricity hole transport layer 150 can be selected according to its kenel, comprises injection method, rubbing method or coating method.Outer surface at solar cell module 100 can cover a silica gel layer (not shown), to protect this solar cell module.In addition, also can use hot pressing mode to encapsulate solar cell module 100, promptly use hot pressing mode that the anode and the negative electrode of solar cell module 100 are bonded together.
Fig. 4 is the entity photo of the concatenation type DSSC module 100 of Fig. 1, and its gross area is 24cm
2, the resultant action area is 8.5cm
2Fig. 5 is the efficient chart of solar cell module after encapsulation of Fig. 4.As shown in Figure 5, the concatenation type DSSC module 100 of accordinging to the first embodiment of the present invention can obtain 5.02% photoelectric conversion efficiency (η), the open circuit voltage (V of 7.35V
OC), the short circuit current (I of 9.21mA
SC) and 0.63 filling rate (FF).Solar cell module 100 according to the first embodiment of the present invention can obtain higher voltage.
Second embodiment
Fig. 6 shows the drawing in side sectional elevation according to the concatenation type DSSC module 200 of the second embodiment of the present invention.DSSC module 200 is a kind of parallel DSSC module.DSSC module 200 comprises: transparency carrier 210, transparent conductive film oxide layer 220, auxiliary electrode 230, the moon/anodic bonding material 240, electric hole transport layer 250, electron transfer layer 260 and electrically-conductive backing plate 270.Transparency carrier 210, transparent conductive film oxide layer 220, auxiliary electrode 230, the moon/anodic bonding material 240, electric hole transport layer 250, electron transfer layer 260 and electrically-conductive backing plate 270 are identical with the definien of first embodiment institute.With the anode of the electrically-conductive backing plate that is formed with electron transfer layer 260 on it 270, and will be formed with the negative electrode of the transparency carrier 210 of transparent conductive film oxide layer 220 on it as DSSC module 200 as DSSC module 200.
The vertical view of the cathode portion of the solar cell module 200 of Fig. 7 a demonstration displayed map 6; And Fig. 7 b shows along the drawing in side sectional elevation of the c-c line of Fig. 7 a.Shown in Fig. 7 a and 7b, the cathode portion of solar cell module 200 comprises transparency carrier 210, transparent conductive film oxide layer 220 and auxiliary electrode 230.The generation type of this cathode portion is: on transparency carrier 210, form transparent conductive film oxide layer (or being called transparent conductive film) 220 earlier; Utilize chemical etching, laser carved or mode (be referred to as and scrape channel process) such as strike off then; On transparent conductive film oxide layer 220, form irrigation canals and ditches 221; On monolithic transparency carrier 210, to obtain to appear the transparent conductive film oxide layer 220 of N separated region (it can form N array pattern); That is, transparent conductive film is changed into a plurality of separated regions by block, then; Utilize modes such as wire mark, plating, electroless plating, electrophoresis, vapor deposition, brush plating, brushing or rotary coating, auxiliary electrode 230 is formed on the edge of the negative electrode of solar cell module 200.Again, masking method also capable of using is made this cathode portion, promptly; Can utilize vacuum adhesive tape or mould earlier; The zone that forms transparent conductive film oxide layer 220 of not expecting on the transparency carrier 210 is covered, and then form transparent conductive film oxide layer 220, then remove vacuum adhesive tape or mould; Can produce zone that is formed with transparent conductive film oxide layer 220 and the zone that is not formed with transparent conductive film oxide layer 220; Then, utilize modes such as wire mark, plating, electroless plating, electrophoresis, vapor deposition, brush plating, brushing or rotary coating, auxiliary electrode 230 is formed on the edge of the negative electrode of solar cell module 200.Then; Through sol-gel process, hydro thermal method, anodizing process, chemical vapour deposition (CVD), physical vapour deposition (PVD), vapor deposition or mode such as electroless plated; On the negative electrode of DSSC module 200, form catalyst layer (not shown); To promote electrochemical reaction, the material of this catalyst layer can be Au (gold), Pd (palladium), Pt (platinum) or carbon (C).
The vertical view of the anode part of the solar cell module 200 of Fig. 8 a displayed map 6; And Fig. 8 b shows along the drawing in side sectional elevation of the d-d line of Fig. 8 a.Shown in Fig. 8 a and 8b, the anode part of solar cell module 200 comprises electron transfer layer 260 and electrically-conductive backing plate 270.This anode part is: preparation can with the corresponding monolithic electrically-conductive backing plate 270 of cathode portion, on the surface of this monolithic electrically-conductive backing plate, formed the zone of a plurality of electron transfer layers 260 that can be complementary with N array pattern.At last; On the negative electrode of DSSC module 200 and the interface between the anode, the moon/anodic bonding material 240 is set and makes negative electrode and anodic bonding together; And the electric hole transport layer 250 contain iodide ion is set between negative electrode and anode; Can accomplish the encapsulation of concatenation type DSSC module 200 and make it have sandwich construction (that is, utilizing Sanming City therapy to encapsulate), as shown in Figure 6.The set-up mode of electricity hole transport layer 250 can be selected according to its kenel, comprises injection method, rubbing method or coating method.Outer surface at solar cell module 200 can cover a silica gel layer (not shown), to protect this solar cell module.In addition, also can use hot pressing mode to encapsulate solar cell module 200, promptly use hot pressing mode that the anode and the negative electrode of solar cell module 200 are bonded together.
Fig. 9 is the entity photo of the concatenation type DSSC module 200 of Fig. 6, and its gross area is 30cm
2, the resultant action area is 12cm
2Figure 10 is the solar cell module after encapsulation of Fig. 9 and the relative efficiency chart of a contrast solar cell module; Wherein (a) line segment is a transparent conductive film oxide layer 220 after excision (promptly; Through blockization) efficiency curve (efficient of the solar cell module of its displayed map 9); And (b) line segment is the efficiency curve (it show the efficient of contrast solar cell module) of transparent conductive film oxide layer 220 without excision (that is, without blockization).Shown in (b) line segment of Figure 10, if the transparent conductive film oxide layer of concatenation type DSSC module 200 220 can obtain photoelectric conversion efficiency (η): open circuit voltage (V 4.10%, during without excision
OC): 0.72V, short-circuit current density (J
SC): 10.20mA cm
-2And filling rate (FF): 0.56.Shown in (a) line segment of Figure 10; With respect to the DSSC module of transparent conductive film oxide layer 220 without excision, transparent conductive film oxide layer 220 can obtain photoelectric conversion efficiency (η) through the DSSC module of excision: open circuit voltage (V 5.04%,
OC): 0.72V, short-circuit current density (J
SC): 12.17mA cm
-2And filling rate (FF): 0.58.Solar cell module 200 according to the second embodiment of the present invention can increase the conduction efficiency of electronics in transparent conductive film oxide layer 220, and then increases the output current of solar cell module.
In sum; According to the present invention; The negative electrode block of solar cell module is changed into a plurality of separated regions, and on one or more anode of solar cell module, form one or more the regional electron transfer layer that to be complementary with a plurality of separated regions of negative electrode, use the moon/anodic bonding material together then negative electrode and anodic bonding; And electric hole transport layer is set between negative electrode and anode, can make solar cell module with serial or parallel connection form.
Though the present invention is with reference to preferred embodiment and graphic explanation in detail; But haveing the knack of this art can understand under the situation of not leaving spirit of the present invention and category; Can carry out various modifications, variation and equivalent substitution, yet these modifications, variation and equivalent substitution fall into still in the appended claim of the present invention.
Claims (44)
1. the structure of an array concatenation type solar cell module comprises:
One transparency carrier;
One transparent conductive film is formed on this transparency carrier, and wherein this transparent conductive film is changed into a plurality of separated regions by block, and will be formed with the negative electrode of this transparency carrier of this transparent conductive film as a solar cell module on it;
One or more electrically-conductive backing plate; Go up an electron transfer layer that forms one or more zone in its surface; Wherein this one or more zone of this electron transfer layer is complementary with these a plurality of separated regions; This electron transfer layer is that how mitron constitutes by the complex root semiconductor, and will be formed with the anode of this electrically-conductive backing plate of this electron transfer layer as this solar cell module on it;
One catalyst layer is formed on this negative electrode;
One auxiliary electrode is formed on the edge of this negative electrode;
One light-sensitive coloring agent is attached to this semiconductor how on the tube wall of mitron; And
One electric hole transport layer is arranged between this negative electrode and this anode.
2. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, the material of this electrically-conductive backing plate is indium (In), zinc (Zn), tin (Sn), titanium (Ti) or tungsten (W).
3. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, how mitron is indium sesquioxide (In to this complex root semiconductor
2O
3), zinc oxide (ZnO), tin ash (SnO
2), titanium dioxide (TiO
2) or tungstic acid (WO
3).
4. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, this auxiliary electrode is conductivity or corrosion stability metal.
5. the structure of array concatenation type solar cell module according to claim 4 is characterized in that this conductivity or corrosion stability metal are copper, gold, platinum, silver, aluminium, nickel, titanium, cobalt, tin, indium or zinc.
6. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, this transparency carrier is a transparent glass substrate or a transparent plastic substrate.
7. the structure of array concatenation type solar cell module according to claim 6; It is characterized in that; This plastic base is by PEN (PEN; Poly (ethylene naphthalate)) or PET (PET, poly (ethylene terephthalate)) made.
8. the structure of array concatenation type solar cell module according to claim 1; It is characterized in that; This transparent conductive film is indium tin oxide (ITO, indium tin oxides), aluminium zinc oxide (AZO, Al-Zn oxides), antimony tin oxide (ATO; Antimony doped tin oxides) or fluorine tin-oxide (FTO, fluorine doped tin oxides).
9. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, the material of this catalyst layer is Au (gold), Pd (palladium), Pt (platinum) or carbon (C).
10. according to the structure of claim 1 or 9 described array concatenation type solar cell modules, it is characterized in that this catalyst layer has island or granular microstructure.
11. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, this light-sensitive coloring agent is organic metal dyestuff, inorganic light-sensitive coloring agent or organic photosensitive dyestuff.
12. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, more comprises:
One plasticity molecular film is arranged on the interface between this anode and this negative electrode.
13. the structure of array concatenation type solar cell module according to claim 12 is characterized in that, this plasticity molecular film is heat shrinkage film, thermosetting film, thermoplastic film, ultraviolet light polymerization film or pellosil.
14. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, the kenel of this electricity hole transport layer comprises: liquid, colloidal state or solid-state.
15. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, more comprises:
One silica gel layer is covered in the outer surface of this solar cell module.
16. the structure of array concatenation type solar cell module according to claim 1 is characterized in that, more comprises: semiconductor is the rice particle how, attached to this semiconductor how in the pipe of mitron.
17. the method for packing of the structure of an array concatenation type solar cell module as claimed in claim 1 comprises the following step:
Should electricity hole transport layer be arranged between this anode and this negative electrode;
This anode and this negative electrode are bonded together, so that this solar cell module has sandwich construction; And
Outer surface at this solar cell module covers a silica gel layer.
18. method for packing according to claim 17; It is characterized in that this step that this anode and this negative electrode are bonded together comprises: on the interface between this anode and this negative electrode, a plasticity molecular film is set and this anode and this negative electrode are bonded together.
19. method for packing according to claim 18 is characterized in that, this plasticity molecular film is heat shrinkage film, thermosetting film, thermoplastic film, ultraviolet light polymerization film or pellosil.
20. method for packing according to claim 17 is characterized in that, this step that this anode and this negative electrode are bonded together comprises: utilize hot pressing mode that this anode and this negative electrode are bonded together.
21. the manufacturing approach of an array concatenation type solar cell module comprises the following step:
On a transparency carrier, form a transparent conductive film;
This transparent conductive film block is changed into a plurality of separated regions, wherein will be formed with the negative electrode of this transparency carrier of this transparent conductive film on it as a solar cell module;
On the surface of one or more electrically-conductive backing plate, form an electron transfer layer in one or more zone; Wherein this one or more zone of this electron transfer layer is complementary with these a plurality of separated regions; This electron transfer layer is that how mitron constitutes by the complex root semiconductor, and will be formed with the anode of this electrically-conductive backing plate of this electron transfer layer as this solar cell module on it;
Make a light-sensitive coloring agent be attached to this semiconductor how on the tube wall of mitron;
One catalyst layer is formed on this negative electrode;
Form an auxiliary electrode at the edge of this negative electrode;
One electric hole transport layer is arranged between this negative electrode and this anode; And
This anode and this negative electrode are bonded together.
22. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that this electron transfer layer is indium sesquioxide (In
2O
3), zinc oxide (ZnO), tin ash (SnO
2), titanium dioxide (TiO
2) or tungstic acid (WO
3).
23. manufacturing approach according to claim 21 or 22 described array concatenation type solar cell modules; It is characterized in that the method that forms this electron transfer layer is sol-gel process, hydro thermal method, method of spin coating, sedimentation, spread coating, anodizing process, chemical vapour deposition technique or physical vaporous deposition.
24. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, the material of this electrically-conductive backing plate is indium (In), zinc (Zn), tin (Sn), titanium (Ti) or tungsten (W).
25. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, make this light-sensitive coloring agent attached to this semiconductor how the method on the tube wall of mitron be infusion method, method of spin coating or drape process.
26. the manufacturing approach of array concatenation type solar cell module according to claim 21; It is characterized in that the method that forms this transparent conductive film is sol-gel process, hydro thermal method, anodizing process, chemical vapour deposition technique or physical vaporous deposition.
27. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, the mode that this transparent conductive film block is changed into a plurality of separated regions is for scraping channel process or masking method.
28. the manufacturing approach of array concatenation type solar cell module according to claim 21; It is characterized in that the method that forms this catalyst layer is vapor deposition, electroless plated, sol-gel process, hydro thermal method, anodizing process, chemical vapour deposition technique or physical vaporous deposition.
29. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, the material of this catalyst layer is Au (gold), Pd (palladium), Pt (platinum) or carbon (C).
30. the manufacturing approach according to claim 21 or 29 described array concatenation type solar cell modules is characterized in that this catalyst layer has island or granular microstructure.
31. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, this light-sensitive coloring agent is organic metal dyestuff, inorganic light-sensitive coloring agent or organic photosensitive dyestuff.
32. the manufacturing approach of array concatenation type solar cell module according to claim 21; It is characterized in that this step that this anode and this negative electrode are bonded together comprises: on the interface between this anode and this negative electrode, a plasticity molecular film is set and this anode and this negative electrode are bonded together.
33. the manufacturing approach of array concatenation type solar cell module according to claim 32 is characterized in that, this plasticity molecular film is heat shrinkage film, thermosetting film, thermoplastic film, ultraviolet light polymerization film or pellosil.
34. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, this step that this anode and this negative electrode are bonded together comprises: use hot pressing mode that this anode and this negative electrode are bonded together.
35. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, the kenel of this electricity hole transport layer comprises: liquid, colloidal state or solid-state.
36. the manufacturing approach of array concatenation type solar cell module according to claim 35 is characterized in that the method that this electricity hole transport layer is set is injection method, rubbing method or coating method.
37. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, more comprises: the outer surface at this solar cell module covers a silica gel layer.
38. the manufacturing approach of array concatenation type solar cell module according to claim 21; It is characterized in that the method that forms this auxiliary electrode is wire mark, galvanoplastic, non-electrolytic plating method, electrophoresis, vapour deposition method, brush plating method, spread coating or method of spin coating.
39. the manufacturing approach according to claim 21 or 38 described array concatenation type solar cell modules is characterized in that this auxiliary electrode is conductivity or corrosion stability metal.
40. the manufacturing approach according to the described array concatenation type of claim 39 solar cell module is characterized in that this conductivity or corrosion stability metal are copper, gold, platinum, silver, aluminium, nickel, titanium, cobalt, tin, indium or zinc.
41. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, more comprises: make semiconductor how the rice particle attached to this semiconductor how in the pipe of mitron.
42. the manufacturing approach of array concatenation type solar cell module according to claim 21 is characterized in that, this transparency carrier is a transparent glass substrate or a transparent plastic substrate.
43. manufacturing approach according to the described array concatenation type of claim 42 solar cell module; It is characterized in that; This plastic base is by PEN (PEN; Poly (ethylene naphthalate)) or PET (PET, poly (ethylene terephthalate)) made.
44. the manufacturing approach of array concatenation type solar cell module according to claim 21; It is characterized in that; This transparent conductive film is indium tin oxide (ITO, indium tin oxides), aluminium zinc oxide (AZO, Al-Zn oxides), antimony tin oxide (ATO; Antimony doped tin oxides) or fluorine tin-oxide (FTO, fluorine doped tin oxides).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010156529A CN102214518B (en) | 2010-04-07 | 2010-04-07 | Structure of array type tandem solar battery module and manufacturing method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010156529A CN102214518B (en) | 2010-04-07 | 2010-04-07 | Structure of array type tandem solar battery module and manufacturing method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102214518A CN102214518A (en) | 2011-10-12 |
| CN102214518B true CN102214518B (en) | 2012-10-10 |
Family
ID=44745788
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201010156529A Expired - Fee Related CN102214518B (en) | 2010-04-07 | 2010-04-07 | Structure of array type tandem solar battery module and manufacturing method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102214518B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201310854D0 (en) * | 2013-06-18 | 2013-07-31 | Isis Innovation | Photoactive layer production process |
| CN104200864B (en) * | 2014-08-25 | 2017-05-03 | 厦门大学 | Isotope battery based on wide bandgap semiconductor nano-tube array film structure |
| CN104576768A (en) * | 2015-01-30 | 2015-04-29 | 东莞佰鸿电子有限公司 | Optical receiver |
| CN113823745B (en) | 2021-11-10 | 2022-04-12 | 浙江晶科能源有限公司 | Solar cell module, preparation method thereof and photovoltaic module |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TW200950115A (en) * | 2008-05-13 | 2009-12-01 | Dongjin Semichem Co Ltd | Dye sensitized solar cell module |
| TW200952231A (en) * | 2008-06-06 | 2009-12-16 | Dc Solar Corp | A large area flexible dye-sensitized solar cell and the electrochemical fabricating method thereof |
| TW201001724A (en) * | 2008-06-30 | 2010-01-01 | Dc Solar Corp | Dye-sensitized solar cell having a double-layer nanotube structure and manufacturing method thereof |
| TW201010108A (en) * | 2008-08-26 | 2010-03-01 | Dc Solar Corp | Large area dye-sensitized solar cell and the thermal spraying fabrication methods thereof |
| CN101682100A (en) * | 2007-06-06 | 2010-03-24 | 株式会社藤仓 | Dye-sensitized solar battery module and method for manufacturing the same |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100481524C (en) * | 2003-09-10 | 2009-04-22 | 大日本印刷株式会社 | Encapsulant layer for solar battery assembly and solar battery assembly |
| JP2005250210A (en) * | 2004-03-05 | 2005-09-15 | Fuji Photo Film Co Ltd | Optical element varying optical density in response to electromagnetic wave |
| KR20090121629A (en) * | 2008-05-22 | 2009-11-26 | 삼성전자주식회사 | Solar cell and solar cell module using the same |
-
2010
- 2010-04-07 CN CN201010156529A patent/CN102214518B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101682100A (en) * | 2007-06-06 | 2010-03-24 | 株式会社藤仓 | Dye-sensitized solar battery module and method for manufacturing the same |
| TW200950115A (en) * | 2008-05-13 | 2009-12-01 | Dongjin Semichem Co Ltd | Dye sensitized solar cell module |
| TW200952231A (en) * | 2008-06-06 | 2009-12-16 | Dc Solar Corp | A large area flexible dye-sensitized solar cell and the electrochemical fabricating method thereof |
| TW201001724A (en) * | 2008-06-30 | 2010-01-01 | Dc Solar Corp | Dye-sensitized solar cell having a double-layer nanotube structure and manufacturing method thereof |
| TW201010108A (en) * | 2008-08-26 | 2010-03-01 | Dc Solar Corp | Large area dye-sensitized solar cell and the thermal spraying fabrication methods thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102214518A (en) | 2011-10-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Hashmi et al. | Review of materials and manufacturing options for large area flexible dye solar cells | |
| Lenzmann et al. | Recent advances in dye‐sensitized solar cells | |
| CN104134711A (en) | Perovskite solar cell and preparation method of perovskite solar cell by solution method | |
| CN107240613A (en) | A kind of unleaded perovskite solar cell | |
| WO2012144534A1 (en) | Capacitor-integrated solar cell having electricity storage function | |
| CN102214518B (en) | Structure of array type tandem solar battery module and manufacturing method thereof | |
| JP5489621B2 (en) | Photoelectric conversion element and photovoltaic device using the photoelectric conversion element | |
| US20070246096A1 (en) | Dye-sensitized solar cell | |
| CN102074376A (en) | Dye-sensitized solar battery | |
| CN102270683A (en) | Integrated flexible thin film solar cell module and method for making same | |
| JP2009009936A (en) | Photoelectric conversion device | |
| CN101488532A (en) | Back electrode module of solar cell | |
| JP2008277422A (en) | Laminated photoelectric converter | |
| CN103426645B (en) | Utilize metal flexible DSSC and the manufacture method thereof of the metal substrate of dual coating | |
| KR101192981B1 (en) | Metal flexible dye-sensitized solar cell and manufacturing method thereof | |
| CN101820004A (en) | Photo-electro separated solar cell back reflector | |
| JP2008244258A (en) | Photoelectric conversion device and photovoltaic generator | |
| JP2009135395A (en) | Photoelectric conversion device, photovoltaic generator, and photoelectric conversion module | |
| KR101220169B1 (en) | Metal flexible dye-sensitized solar cell with coating metal substrate for processing polishing and manufacturing method thereof | |
| KR20110077923A (en) | Front electrode for a thin film silicone solar cell and a thin film silicone solar cell comprising the same | |
| RU2384916C1 (en) | Photoactive element | |
| JP5153248B2 (en) | Photoelectric conversion device and photovoltaic power generation device | |
| JP2009009851A (en) | Photoelectric conversion device | |
| KR101422509B1 (en) | Metal flexible dye-sensitized solar cell with texturing azo glass transparent electrode and manufacturing method thereof | |
| KR101212938B1 (en) | Metal flexible dye-sensitized solar cell with metal substrate for processing polishing and manufacturing method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121010 Termination date: 20170407 |